Airplane steering wheel multi-axis force measurement component and measurement method thereof

A technology for measuring components and steering wheels, which is applied in the field of aeronautical engineering testing and testing, can solve problems such as difficulty in on-site installation and use, large vertical and horizontal dimensions, and large space occupation, and achieves compact structure, small space size, and high testing accuracy Effect

Active Publication Date: 2014-12-24
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Abstract
  • Description
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  • Application Information

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Problems solved by technology

In the above measurement line of sight, the vertical and horizontal dimensions are large, which takes up a lot of space and brings great difficulties to on-site installation and use.

Method used

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  • Airplane steering wheel multi-axis force measurement component and measurement method thereof
  • Airplane steering wheel multi-axis force measurement component and measurement method thereof
  • Airplane steering wheel multi-axis force measurement component and measurement method thereof

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Embodiment Construction

[0024] Below in conjunction with accompanying drawing and embodiment the present invention is described in further detail:

[0025] The structure of this embodiment is as figure 2 , the first vertical force signal detection unit [3] and the second vertical force signal detection unit [5] are symmetrical to the center line of the installation connection unit [4], respectively arranged on both sides of the installation connection unit [4]; the first horizontal force The signal detection unit [2] and the second horizontal force signal detection unit [6] are also symmetrical to the center line of the installation connection unit [4], and are respectively arranged on the first vertical force signal detection unit [3] and the second vertical force signal detection unit Both sides of [5]; the first control handle [1] and the second control handle [7] are also symmetrical to the center line of the installation connection unit [4], and are respectively arranged on the first horizontal...

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Abstract

The invention discloses an airplane steering wheel multi-axis force measurement component and a measurement method thereof, which belong to the aeronautical engineering test detection field. The measurement component consists of a control handle, a horizontal force signal detection unit, a vertical force signal detection unit and an installation connection unit, which are combined horizontally in turn. The force signal detection units and the control handle are respectively arranged at the two sides of the installation connection unit which serves as the center. The control handle is arranged at the outmost end and the two ends of the force signal detection units are respectively connected with the installation connection unit and the control handle. The measurement component is connected with the steering wheel through the installation connection unit. Control force is exerted onto the steering wheel through the control handle and controls the movement of the steering wheel. The force signal detection units measure the control force. The invention has the advantages of compact and simple structure, reliable work, high measurement precision and convenient installation, use and adjustment, accords with the actual control situation of the airplane steering wheel and is applicable to the measurement of the control force of various airplane steering wheels.

Description

technical field [0001] The invention belongs to the field of aeronautical engineering test and detection, in particular to an aircraft steering wheel multi-dimensional force measurement component and a measurement method thereof. Background technique [0002] At present, in the measurement of aircraft steering wheel force, it is often to complete the measurement of the steering wheel force by modifying it for a specific steering wheel; Disk force. There are following deficiencies: [0003] 1. To modify a specific steering wheel, it is necessary to design and complete the steering wheel force measurement unit according to the structure of the steering wheel, and combine it with the steering wheel as a part of the steering wheel. The result of the transformation of the steering wheel may affect the original functional characteristics such as the strength of the steering wheel. On the other hand, the process of modifying the aircraft steering wheel is complicated and difficul...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01L5/22
Inventor 支超有薛峰高承雍
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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